View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68640U 26144.77924169 +.00000000 +00000-0 -27838+1 0 00008
2 68640 88.9869 323.4172 0011434 75.0559 285.1865 13.63894363 01
| Epoch (UTC): | 24 May 2026 18:42:06 |
| Eccentricity: | 0.0011434 |
| inclination: | 88.9869° |
| perigee height: | 1013 km |
| apogee height: | 1030 km |
| right ascension of ascending node: | 323.4172° |
| argument of perigee: | 75.0559° |
| revolutions per day: | 13.63894363 |
| mean anomaly at epoch: | 285.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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